View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 54880U 26145.48103390 +.00000000 +00000-0 +14864-4 0 00001
2 54880 139.3352 235.2502 0007207 177.0999 182.9850 15.10681461 06
| Epoch (UTC): | 25 May 2026 11:32:41 |
| Eccentricity: | 0.0007207 |
| inclination: | 139.3352° |
| perigee height: | 529 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 235.2502° |
| argument of perigee: | 177.0999° |
| revolutions per day: | 15.10681461 |
| mean anomaly at epoch: | 182.9850° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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